South Windsor, CT, United States of America

Shankar S Magge

This inventor holds 24 USPTO granted patents and 8 published patent applications, plus 1 CIPO patent and 6 EPO patents, primarily in Gas Turbine Engineering. Top assignees: United Technologies Corporation, Raytheon Technologies Corporation. Active years: 2006-2023.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Shankar S Magge. Retrieved from https://idiyas.com/inventor/shankar-s-magge

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

USPTO Granted Patents = 24 

% Patents Active = 100.0


 

Average Co-Inventor Count = 4.7

ph-index = 10

Forward Citations = 243(Granted Patents)


Location History:

  • S. Windsor, CT (US) (2011 - 2015)
  • South Windsor, CT (US) (2006 - 2023)

Company Filing History:


Years Active: 2006-2023

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Areas of Expertise:
Gas Turbine Engine
High Bypass Turbofan
Centrifugal Compressor
Turbine Section
Aerodynamic Shape
Vane Arrangement
Flow Turning Features
Counter Rotating Turbine
Airfoil Profile
Vane Throat Areas
Low Pressure Turbine
Splitter Gear System
24 patents (USPTO):Explore Patents

Title: **Innovative Contributions of Shankar S. Magge in Gas Turbine Technologies**

Introduction

Shankar S. Magge, based in South Windsor, CT, is an accomplished inventor with a remarkable portfolio of 24 patents. His expertise lies predominantly in the field of gas turbine engines, where he has made significant advancements that enhance performance and efficiency.

Latest Patents

Among his latest innovations, Shankar has developed a patent for the turbine section of a gas turbine engine. This invention features a propulsor that includes a circumferential array of blades and a low pressure compressor section with an inlet annulus area. This design positions the maximum gas path radius in relation to the maximum radius of blades at a precise ratio of greater than or equal to 0.35 and less than 0.55. Additionally, he has contributed to a turbine section of a high bypass turbofan engine. This advanced turbine comprises a fan with rotatable blades, a comprehensive compressor system, and a turbine featuring both high and low pressure sections, where the maximum gas path radius is maintained at a ratio of less than 0.6 compared to the maximum radius of the fan blades.

Career Highlights

Shankar S. Magge has garnered extensive experience through his tenure at significant organizations in the aerospace industry. Notably, he has worked at United Technologies Corporation and Raytheon Technologies Corporation, both of which are renowned for their innovative contributions to technology.

Collaborations

Throughout his career, Shankar has collaborated with notable colleagues, including Gabriel L. Suciu and Paul R. Adams. These professional relationships have likely fostered an environment of creativity and innovation, leading to the development of cutting-edge technologies in gas turbine engineering.

Conclusion

Shankar S. Magge exemplifies the spirit of innovation within the engineering community. His extensive patent portfolio and contributions to gas turbine technologies underscore his commitment to advancing the field. As he continues to work on cutting-edge solutions, his impact on the aerospace industry is poised to grow even further.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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